Airworthiness Directives; Rolls-Royce plc RB211-22B, RB211-524, and RB211-535 Series Turbofan Engines

---
identifier: "/us/fr/04-21912"
source: "fr"
legal_status: "authoritative_unofficial"
title: "Airworthiness Directives; Rolls-Royce plc RB211-22B, RB211-524, and RB211-535 Series Turbofan Engines"
title_number: 0
title_name: "Federal Register"
section_number: "04-21912"
section_name: "Airworthiness Directives; Rolls-Royce plc RB211-22B, RB211-524, and RB211-535 Series Turbofan Engines"
positive_law: false
currency: "2004-09-30"
last_updated: "2004-09-30"
format_version: "1.1.0"
generator: "[email protected]"
agency: "Transportation Department"
document_number: "04-21912"
document_type: "rule"
publication_date: "2004-09-30"
agencies:
  - "Transportation Department"
  - "Federal Aviation Administration"
cfr_references:
  - "14 CFR Part 39"
rin: "2120-AA64"
fr_citation: "69 FR 58257"
fr_volume: 69
docket_ids:
  - "Docket No. 2003-NE-57-AD"
  - "Amendment 39-13798"
  - "AD 2004-19-04"
effective_date: "2004-09-30"
fr_action: "Final rule; correction."
---


#  [Corrected]

**AGENCY:**

Federal Aviation Administration, DOT.

**ACTION:**

Final rule; correction.

**SUMMARY:**

This document makes a correction to Airworthiness Directive (AD) 2004-19-04. That AD applies to Rolls-Royce plc (RR) RB211-22B, RB211-524, and RB211-535 series turbofan engines. That AD was published in the *Federal Register* on September 22, 2004 (69 FR 56683). In the amendatory language, under § 39.13 [Amended], the amendment number for the AD was inadvertently omitted. This document corrects that omission. In all other respects, the original document remains the same.

**EFFECTIVE DATE:**

Effective September 30, 2004.

**FOR FURTHER INFORMATION CONTACT:**

Christopher Spinney, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803-5299; telephone (781) 238-7175, fax (781) 238-7199.

**SUPPLEMENTARY INFORMATION:**

A final rule AD, FR Doc. 04-21173 that applies to RR RB211-22B, RB211-524, and RB211-535 series turbofan engines, was published in the *Federal Register* on September 22, 2004 (69 FR 56683). The following correction is needed:

**14 CFR Part 39**

§ 39.13

On page 56684, in the second column, under § 39.13 [Amended], in the fifth line, “2004-19-04 Rolls-Royce plc: Docket No.” is corrected to read “2004-19-04 Rolls-Royce plc: Amendment 39-13798. Docket No.”.

Issued in Burlington, MA, on September 23, 2004.

Francis A. Favara,

Acting Manager, Engine and Propeller Directorate, Aircraft Certification Service.